View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 63140U 26145.36181275 +.00000000 +00000-0 +14843-2 0 00000
2 63140 43.0017 148.2924 0002989 263.6974 96.3554 15.70938906 06
| Epoch (UTC): | 25 May 2026 08:41:00 |
| Eccentricity: | 0.0002989 |
| inclination: | 43.0017° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 148.2924° |
| argument of perigee: | 263.6974° |
| revolutions per day: | 15.70938906 |
| mean anomaly at epoch: | 96.3554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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